N962SW

Service difficulty reports · 173

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N962SW' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWIA200820427Floorbeam · crackedC-CHECK, FS 280 RBL9 AND LBL9 UPPER FLOOR SUPPORT CRACKED. REPAIRED PER REO.Aug 21, 2008 · N962SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200820426Floorbeam · crackedC-CHECK, FS 280 RBL9 LOWER FRAME CRACKED. REPAIRED PER REO.Aug 21, 2008 · N962SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200718652Unknown · odorFLT 5860 - FLIGHT ATTENDANT REPORTS BURNING SMELL IN GALLEY. INSPECTED GALLEY HEAT, FAN, LIGHTS AND POTABLE WATER SYSTEM. COULD NOT DUPLICATE BURNING SMELL.Aug 27, 2007 · N962SW · Cndair CL6002B19 · Buffet/GalleysSDR SWIA200617432Acm · odorFA REPORTS SMOKE ODOR AFTER TAKEOFF. REPLACED RIGHT ACM IAW MM 21-51-10. OPERATIONAL CHECKS GOOD, SN OFF: 200212012.Dec 11, 2006 · N962SW · Cndair CL6002B19 · Cabin Cooling SystemSDR SWIA200617588Intercostal · crackedPASSENGER DOOR, CRACKED INTERCOSTAL AFT SIDE OF DOOR INSIDE OF THE 2ND ACCESS HOLE FROM BOTTOM, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED AND SEALED NEW INTERCOSTAL ON AFT SIDE OF DOOR INSIDE OF THE 2ND ACCESS HOLE FROM BOTTOM OF PAX DOOR IAW CRJ200 SRMNov 14, 2006 · N962SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200617587Step · crackedPAX DOOR FWD WEB BETWEEN 4TH AND 5TH STEP HAS CRACK IN RADIUS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS AT PAX DOOR FWD WEB BETWEEN 4TH 5TH STEPS PER REO 601R 52-11-702.Nov 14, 2006 · N962SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200617586Step · crackedPAX DOOR AFT WEB BETWEEN 4TH AND 5TH STEP HAS CRACK IN RADIUS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER BOMBARDIER REO 601R-52-11-702.Nov 14, 2006 · N962SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200616629Trim Switch · intermittentCREW REPORTS AILERON TRIM SWITCH ONLY WORKS IN RWD POSITION LWD POSITION IS INTERMITTENT. REPLACED AIL/RUD TRIM PANEL. OPERATIONAL CHECK GOOD.Apr 22, 2006 · N962SW · Cndair CL6002B19 · Aileron Tab Control SystemSDR SWIA200616089Trim Switch · malfunctionedCAPT STAB TRIM WON'T TRIM NOSE UP. REPLACED PITCH TRIM SWITCH CAPT SIDE IAW AMM 27-41-05. OPERATIONAL CHECK GOOD.Jan 4, 2006 · N962SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200515999Computer · malfunctionedIN CLIMB, WHILE ON FO SIDE, AUTO PILOT AND YAW DAMP DISENGAGED. REPLACED NR 2 FCC CARD IAW AMM 22-00-00. OPERATIONAL CHECK GOOD.Dec 11, 2005 · N962SW · Cndair CL6002B19 · Autopilot SystemSDR SWIA200515889Pcu · malfunctionedSPOILERON FAULT STATUS MSG ON APPROACH TO SLC. REPLACED LEFT SPOILERON OUTBOARD PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD. P/N ON 27000-7, OFF 7750.Nov 18, 2005 · N962SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200515870Windshield · crackedFO'S FRONT WINDSHIELD SHATTERED ON DESCENT. REPLACED FO'S FRONT WINDOW.Nov 15, 2005 · N962SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200515834Control Unit · malfunctionedRECEIVED IB GROUND SPL CAUTION MSG. REPLACED NR 2 SECU IAW MM 27-61-05. OPERATIONAL CHECK GOOD.Nov 10, 2005 · N962SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200515693Pcu · malfunctionedSPOILERON FAULT MESSGAE DISPLAYED ON APPROACH TO SLC. REPLACED RT INBOARD AND OUTBOARD SPOILERON PCU IAW AMM 27-62-01. OPERATIONAL CHECK GOOD.Oct 16, 2005 · N962SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200515538Flap System · intermittentON APPROACH FLAPS FAIL MESSAGE DISPLAYED AT 8 DEGREES. RESET FLAP SYSTEM AND PERFORMED FLAP SYSTEM TEST. OPERATIONAL CHECK GOOD.Sep 14, 2005 · N962SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200515273Attach Angle · crackedFUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH ANGLE IS CRACKED, OUTBOARD SIDE FS280.00 RBL 9.0. REPLACED ATTACH ANGLE IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-21-11, 51-42-13.Apr 22, 2005 · N962SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA200515272Attach Angle · crackedFUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH ANGLES ARE CRACKED. INBOARD AND OUTBOARD; FS 280.00; LBL - 9.0. REPLACED ATTACH ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00, 51-42-21, 51-25-16, 51-21-11, 57-42-13.Apr 22, 2005 · N962SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA200514805Servo · malfunctionedAFTER A/P DISCONNECT ON FINAL, F/O UNABLE TO MOVE ELEVATOR IN EITHER DIRECTION FOR 5 TO 7 SECONDS AFTER DISC PITCH CONTROL THEN RETURNED TO NORMAL. REPLACED ELEVATOR SERVO & SERVO MOUNT UNITS IAW 22-11-14, AND 22-11-24. OPERATIONAL CHECK GOOD. P/N 622-5027-Mar 27, 2005 · N962SW · Cndair CL6002B19 · Autopilot Trim ServoSDR SWIA200414153Pcu · malfunctionedSPOILERON FAULT STATUS MESSAGE ON ED NR 2. REMOVED AND REPLACED RIGHT OUTBOARD SPOILERON PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD.Nov 28, 2004 · N962SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200414024Control Unit · malfunctionedSPOILERON FAULT MESSAGE CAME ON IN FLIGHT. REMOVED AND REPLACED SECU NR 2 IAW MM 27-61-15. OPERATIONAL CHECK GOOD.Oct 26, 2004 · N962SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200413005Vane · failedAFTER TAKEOFF, STALL FAIL MSG CAME ON. STAYED ON FOR DURATION OF FLIGHT. BOTH AIRSPEED INDICATORS ARE THE SAME. LEFT LOWER RED FLAP INDICATES HIGHER THAN RIGHT SIDE. REMOVED AND REPLACED LEFT AOA VANE WITH A SERVICEABLE UNIT. OPS CHECKS GOOD. COMPLETED IMar 6, 2004 · N962SW · Cndair CL6002B19 · Stall Warning SystemSDR SWIA200412988Computer · malfunctionedSTALL FAIL MESSAGE. REMOVED AND REPLACED STALL PROTECTION COMPUTER IAW CRJ MM 27-34. OPS CHECKS GOOD. STALL FAIL LIGHT ILLUMINATED LATER IN THE DAY AND STAYED ON FOR DURATION OF THE FLIGHT. CHECKED ASSOCIATED WIRING BEHIND STALL PROTECTION COMPUTER. NO DEMar 5, 2004 · N962SW · Cndair CL6002B19 · Stall Warning SystemSDR SWIA200312641Control Unit · malfunctionedFLAPS FAIL MESSAGE INFLIGHT WITH FLAPS SELECTOR AT 8. FOLLOWED QRH AND LANDED FLAPS 8. REMOVED AND REPLACED FECU IAW CRJ MM 27-50-00. OPS CHECK GOOD.Nov 27, 2003 · N962SW · Cndair CL6002B19 · Trailing Edge Flap Control System
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